Shear strength explained

In engineering, shear strength is the strength of a material or component against the type of yield or structural failure when the material or component fails in shear. A shear load is a force that tends to produce a sliding failure on a material along a plane that is parallel to the direction of the force. When a paper is cut with scissors, the paper fails in shear.

In structural and mechanical engineering, the shear strength of a component is important for designing the dimensions and materials to be used for the manufacture or construction of the component (e.g. beams, plates, or bolts). In a reinforced concrete beam, the main purpose of reinforcing bar (rebar) stirrups is to increase the shear strength.

Equations

\tau

applies

\tau=

\sigma1-\sigma3
2

,

where

\sigma1

is major principal stress and

\sigma3

is minor principal stress.

In general: ductile materials (e.g. aluminum) fail in shear, whereas brittle materials (e.g. cast iron) fail in tension. See tensile strength.

To calculate:

Given total force at failure (F) and the force-resisting area (e.g. the cross-section of a bolt loaded in shear), ultimate shear strength (

\tau

) is:

\tau=

F
A

=

F
\pi
2
r
bolt

=

4F
\pi
2
d
bolt

For average shear stress

\tauavg=

V
A

where

\tauavg

is the average shear stress,

V

is the shear force applied to each section of the part, and

A

is the area of the section.[1]

Average shear stress can also be defined as the total force of

V

as

V=\int\taudA

This is only the average stress, actual stress distribution is not uniform. In real world applications, this equation only gives an approximation and the maximum shear stress would be higher. Stress is not often equally distributed across a part so the shear strength would need to be higher to account for the estimate.[2]

Comparison

As a very rough guide relating tensile, yield, and shear strengths:[3]

MaterialUltimate Strength RelationshipYield Strength Relationship
SteelsUSS = approx. 0.75*UTSSYS = approx. 0.58*TYS
Ductile IronUSS = approx. 0.9*UTSSYS = approx. 0.75*TYS .
Malleable IronUSS = approx. 1.0*UTS
Wrought IronUSS = approx. 0.83*UTS
Cast IronUSS = approx. 1.3*UTS
AluminumsUSS = approx. 0.65*UTSSYS = approx. 0.55*TYS
USS: Ultimate Shear Strength, UTS: Ultimate Tensile Strength, SYS: Shear Yield Stress, TYS: Tensile Yield Stress

There are no published standard values for shear strength like with tensile and yield strength. Instead, it is common for it to be estimated as 60% of the ultimate tensile strength. Shear strength can be measured by a torsion test where it is equal to their torsional strength.[4] [5]

When values measured from physical samples are desired, a number of testing standards are available, covering different material categories and testing conditions. In the US, ASTM standards for measuring shear strength include ASTM B769, B831, D732, D4255, D5379, and D7078. Internationally, ISO testing standards for shear strength include ISO 3597, 12579, and 14130.[7]

See also

Notes and References

  1. Book: Hibbeler, Russell. Mechanics of materials. 9 November 2017 . Pearson Education . 978-1-292-17828-8. 1014358513.
  2. Web site: Mechanics eBook: Shear and Bearing Stress. www.ecourses.ou.edu. 2020-02-14.
  3. Web site: Shear Strength of Metals. www.roymech.org.
  4. Web site: Shear Strength - Instron. www.instron.us. 2020-02-14. 2020-02-14. https://web.archive.org/web/20200214030206/https://www.instron.us/en-us/home/our-company/library/glossary/s/shear-strength. dead.
  5. Web site: Calculating Yield & Tensile Strength. Portl. Portl. bolt com. Portland Bolt. en-US. 2020-02-14. Bolt. Company. Manufacturing. St. Inc 3441 NW Guam. Portl. PT547-6758. OR 97210 USA Hours: Monday-Friday 6 AM to 5 PM. 10 October 2011 .
  6. Mechanical Properties of E293/1581 Fiberglass-Epoxy Composite and of Several Adhesive Systems. DC. Watson. May 1982. 24 October 2013. Air Force Wright Aeronautical Laboratories. Wright-Patterson Air Force, Ohio. 16. 24 October 2018. https://web.archive.org/web/20181024073657/http://www.dtic.mil/dtic/tr/fulltext/u2/a117902.pdf. live.
  7. S. Grynko, "Material Properties Explained" (2012),, p. 38.